NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be
1 Item − Article
4. Remarks or Exceptions − Remarques ou exceptions
−20−7 FLT COMPT GASPERS
(Small and Large) C 4 0 May be inoperative provided comfort level isacceptable to the pilot. −20−8 Aft Baggage Compartment
Vent Valves
1) Inlet and outlet vent
valves C 2 0 (M) May be inoperative in closed position provided:a) Inlet and outlet valves (shut off valves) are deactivated,
b) VENT VALVE INLT and VENT VALVE OUTLT CLOSED advisory lights are verified illuminated prior to each flight, and
c) Live animals are not carried.
C 2 0 May be inoperative in open position provided: a) The baggage compartment is empty or, for
ballast purpose, use of bags (made of glass fiber or Kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.
2) VENT VALVE INLT and VENT VALVE OUTLT CLOSED advisory lights
C 2 0 May be inoperative in open position provided: a) The baggage compartment is empty or, for
ballast purpose, use of bags (made of glass fiber or Kevlar) of sand or ingots of non−magnetic metals (such as lead) is acceptable.
−30−1 CABIN PRESS Warning
Light C 1 0 May be inoperative provided flight is conducted at orbelow 10,000 feet MSL, per AFM Supplement 113, UNPRESSURIZED FLIGHT − BLEED ON.
−30−2 Cabin ALT Indicator C 1 0 (O) May be inoperative provided:
a) The Cabin DIFF Pressure Indicator is verified operative, and
b) A chart is provided to convert cabin differential pressure to cabin altitude.
D 1 0 (O) May be inoperative provided flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113, UNPRESSURIZED FLIGHT − BLEED ON.
21−2 Rev 7 Sep 09/2015
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
21 AIR CONDITIONING (CONT’D)
−30−3 Cabin DIFF Pressure
Indicator C 1 0 (O) May be inoperative provided:a) The Cabin ALT Indicator is verified operative, and
b) A chart is provided to convert cabin altitude to cabin differential pressure.
D 1 0 (O) May be inoperative provided flight is conducted in an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113, UNPRESSURIZED FLIGHT − BLEED ON.
−30−4 Cabin RATE Indicator C 1 0 May be inoperative provided all other instruments and functions of the Pressurization System are operative. D 1 0 (O) May be inoperative provided flight is conducted in
an unpressurized configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113, UNPRESSURIZED FLIGHT − BLEED ON.
−30−5 Cabin Pressure Control System
1) AUTO and MAN Modes A 2 0 (M)(O) May be inoperative provided:
a) The FWD OUTFLOW valve and DUMP functions are verified operative,
b) The AFT OUTFLOW valve is verified open, c) The flight is conducted in an unpressurized
configuration, at or below 10,000 feet MSL, in accordance with AFM Supplement 113, UNPRESSURIZED FLIGHT − BLEED ON, and d) Repairs are made within three flight days. 2) AUTO Mode A 1 0 (M) May be inoperative provided:
a) MAN control is verified operative,
b) The FWD OUTFLOW control and the DUMP function are verified operative,
c) Cabin RATE Indicator, Cabin ALT Indicator, and Cabin DIFF Pressure Indicator are verified operative, and
d) Repairs are made within three flight days. Rev 7 Sep 09/2015 21−3
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
21 AIR CONDITIONING (CONT’D)
3) MAN Mode C 1 0 (M) May be inoperative provided: a) AUTO control is verified operative,
b) The FWD OUTFLOW control and the DUMP function are verified operative,
c) Cabin RATE Indicator, Cabin ALT Indicator, and Cabin DIFF Pressure Indicator are verified operative.
−30−6 Aft Valves
1) Aft Outflow Valve C 1 0 (M)(O) May be inoperative provided:
a) The AFT OUTFLOW valve is verified open, and b) Flight is conducted in an unpressurized
configuration, at or below 10,000 feet MSL, in accordance with AFM, Section 4, Paragraph 4.16.7.
2) Aft Safety Valve C 1 0 (M)(O) May be inoperative provided:
a) The AFT OUTFLOW valve is verified open, and b) Flight is conducted in an unpressurized
configuration, at or below 10,000 feet MSL, in accordance with AFM, Section 4, Paragraph 4.16.7.
−50−1 Air Cycle Machines (ACM) C 2 1 May be inoperative provided the associated PACKS switch is selected and remains OFF.
−50−2 Turbine Shut−Off Valves C 2 1 (M#) May be inoperative provided:
a) Turbine Shut−Off Valve is secured in the closed position, and
b) Associated PACKS switch is selected and remains OFF.
−50−3 Pack Bypass Valve C 2 1 (M#) May be inoperative provided:
a) Pack Bypass Valve is locked in the closed, position, and
b) Associated PACKS switch is selected and remains OFF.
−55−1 Aft Baggage Compartment
Vent Valves Deleted. Refer to item 21−20−8.
21−4 Rev 6 Mar 26/2014
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
21 AIR CONDITIONING (CONT’D)
−60−1 CABIN TEMP CONTROL
1) AUTO and MAN Modes C 1 0 (M) May be inoperative provided:
a) The associated CABIN PACK is considered inoperative and is selected and remains OFF, and
b) FLT COMP TEMP CONTROL is verified operative.
2) AUTO Mode C 1 0 (M) May be inoperative provided:
a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative. 3) MAN Mode C 1 0 (M) May be inoperative provided AUTO control is
verified operative.
−60−2 DUCT TEMP GAUGE C 1 0 May be inoperative provided Flight Attendant Temperature Control is operative and flights are conducted in accordance with AFM supplement 85, Operation with inoperative CAB DUCT/CABIN/FC Duct Gauge.
1) CABIN Temperature C 1 0 May be inoperative provided Flight Attendant Temperature Control is operative.
2) CAB DUCT
Temperature C 1 0 May be inoperative provided flights are conducted inaccordance with AFM supplement 85, Operation with Inoperative CAB DUCT/CABIN/FC Duct Gauge. 3) FC DUCT Temperature C 1 0 May be inoperative provided flights are conducted in
accordance with AFM supplement 85, Operation with Inoperative CAB DUCT/CABIN/FC Duct Gauge. −60−3 FLT COMP TEMP
CONTROL
1) AUTO and MAN Modes C 2 0 (M) Both may be inoperative provided:
a) The associated FLT COMP PACK is considered inoperative and is selected and remains OFF, and
b) CABIN TEMP CONTROL (AUTO & MANUAL) is verified operative.
Rev 7 Sep 09/2015 21−5
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
21 AIR CONDITIONING (CONT’D)
2) AUTO Mode C 1 0 (M) May be inoperative provided:
a) MAN control is verified operative, and b) DUCT TEMP indicator is verified operative. 3) MAN Mode C 1 0 (M) May be inoperative provided AUTO control is
operative. −60−4 Flight Attendant Control
Panel − Cabin Temperature Control and CABIN TEMP indication
C − 0 One or all functions/indications may be inoperative provided cabin temperature control is available from the flight deck.
NOTE:
Flight Attendant control of cabin temperature is not available if MANUAL cabin temperature control is selected in the cockpit.
21−6 Rev 6 Mar 26/2014
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
21 AIR CONDITIONING (CONT’D)
22 AUTOMATIC FLIGHT CONTROL
−10−1 A/P DISENG Annunciators
(Glareshield) C 2 1 May be inoperative.
C 2 0 May be inoperative provided autopilot is not used. −10−2 Autopilot
1) Autopilot B 1 0 Any mode functioning normally may be used. 2) Autopilot Pitch Trim
System (AP PITCH TRIM FAIL)
B 1 0 May be inoperative provided: a) Manual pitch trim is operative,
b) Autopilot is considered inoperative and not used, and
c) Flap Auto Pitch Trim (AUTO TRIM FAIL) is considered inoperative and not used. −10−3 Tactile Control Steering
(TCS) Switches C 2 0 May be inoperative.
D 2 1 May be inoperative on the pilot not flying side. −10−4 Flight Guidance Control
Panel (FGCP) C 1 1 Individual modes of operation may be inoperativeprovided that heading bugs, nav source selectors and course selection functions are operative.
Flight Guidance Control Panel Indicators (AP, HSI SEL only)
C 4 0 May be inoperative.
−10−5 Yaw Damper System B 1 0 (M) May be inoperative. NOTE:
Autopilot will not be available.
−10−6 A/P DIS Switches B 2 0 May be inoperative provided the Autopilot is considered inoperative and not used. C 2 1 One may be inoperative provided:
a) The Autopilot is not used below 1,000 ft. AGL, b) Approach minimums do not require the use of
the autopilot, and
c) The pilot flying has the operative disconnect. Rev 6 Mar 26/2014 22−1
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION
−10−1 Communication Systems Transmitters and Receivers (VHF, HF and UHF)
D − 2 Any in excess of those required by regulations and not powered by an essential bus may be inoperative. −10−2
***
“Flitefone (or equivalent)”System D 1 0 (M) May be inoperative. −20−1***
SELCAL System C 1 0 (O) May be inoperative provided alternate proceduresare established and used. D 1 0 May be inoperative provided procedures do notrequire its use. −20−2
***
Aircraft CommunicationsAddressing and Reporting System (ACARS)C 1 0 (O) May be inoperative provided alternate procedures are established and used.
D 1 0 May be inoperative provided routine procedures do not require its use.
ACARS Printer C 1 0 (M)(O) May be inoperative provided the printer is deactivated and secured, and alternate procedures are established and used.
D 1 0 May be inoperative provided routine procedures do not require its use.
−30−1 Alerting System (CHIME/LIGHT) 1) Passenger Configuration
a) Flight Deck Call Light B 2 0 May be inoperative provided the flight deck chime is operative.
b) Flight Deck EMER Light B 2 0 May be inoperative provided the flight deck chime is operative.
c) Flight Deck PA Light B 2 0 May be inoperative provided the flight deck chime is operative.
Rev 7 Sep 09/2015 23−1
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
d) Flight Attendant Call
Light B 2 0 May be inoperative provided:a) The PA system is operative, and
b) Affected alert is not used for lavatory smoke detector alerting.
e) Flight Attendant EMER
Light B 2 0 May be inoperative provided:a) The PA system is operative, and
b) Affected alert is not used for lavatory smoke detector alerting.
f) Flight Attendant PA
Light B 2 0 May be inoperative provided:a) The PA system is operative, and
b) Affected alert is not used for lavatory smoke detector alerting.
g) Flight Attendant Chime B − 0 May be inoperative provided:
a) The PA system is operative, and
b) Affected alert is not used for lavatory smoke detector alerting.
2) Cargo Configuration
Flight Deck Call Light B 2 0 May be inoperative provided the flight deck chime is operative.
−30−2 Pre−Recorded
Announcement (Passenger Briefing) System
C 1 0 (O) May be inoperative provided alternate procedures are established and used.
All Cargo Operations D 1 0 May be inoperative provided all crew members are in the flight compartment.
23−2 Rev 7 Sep 09/2015
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION (CONT’D)
−30−3 PACIS (Passenger Address and Cabin Interphone System)
Passenger Address System
1) Passenger
Configuration B 1 0 (O) May be inoperative provided:a) Alternate procedures are established and used, b) Flight deck/cabin interphone (two way) with
associated calls (e.g. chimes) is operative, and c) Megaphone(s) is/are readily available and
operative. NOTE:
Any station that operates normally may be used.
Rev 7 Sep 09/2015 23−3
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION (CONT’D)
2) Non−Passenger
Configuration A 1 0 (O) May be inoperative for non−passenger carryingoperations for one flight day provided: a) Crew members are the only occupants of the
aircraft, and
b) Alternate procedures are established and used. 3) Cargo Configuration D 1 0 (O) May be inoperative provided all crew members
are on the flight deck. Cabin Interphone System
1) Passenger Configuration
Flight Deck / Cabin and
Cabin / Cabin B 1 1 (O) May be inoperative provided:a) An operative flight deck/cabin interphone (two way) is at an operative flight attendant seat, and b) Alternate communications procedures between
the affected flight attendant station(s) are established and used.
A 1 0 (O) May be inoperative for non− passenger carrying operations for one flight day provided:
a) Crew members are the only occupants of the aircraft, and
b) Alternate procedures are established and used.
23−4 Rev 7 Sep 09/2015
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION (CONT’D)
2) Cargo Configuration Flight Deck / Cabin and
Cabin / Cabin D 1 0 May be inoperative provided all crew members are onthe flight deck. −30−4 Active Noise and Vibration
Suppression System D 1 0 (M) May be inoperative.NOTE:
Aircraft may be dispatched with system operative in the DEGRADED mode with ANVS SYS
DEGRADED lamp illuminated on the Maintenance Panel.
−40−1 Service Interphone System (Flight Compartment to Ground Crew)
C 1 0 May be inoperative provided alternate procedures are established and used.
D 1 0 May be inoperative provided procedures are not dependent on its use.
−50−1 Boom Microphone Push−
To−Talk (PTT) Switches C 4 2 (M) May be inoperative provided one switch at eachpilot’s position is verified operative. −50−2 Headsets D − 2 One required at each pilot’s station.
−50−3 Flight Compartment
Speakers C 2 0 May be inoperative provided:a) Procedures are not dependent on their use, b) Headsets are installed and used by each person
on flight deck duty,
c) All aural alerts, messages and other communication which are normally routed through the flight deck speakers must be audible through headsets, and
d) A spare headset must be readily available for crew use.
−50−4 Boom Microphones (incl.
Headset mics) A − − May be inoperative provided:a) The Flight Data Recorder (FDR) operates normally, and
b) Repairs are made within three flight days. −50−5 Cockpit Handheld
Microphones C 2 0 May be inoperative provided associated boommicrophones are operative. Rev 7 Sep 09/2015 23−5
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION (CONT’D)
−50−6 Cabin Handsets B 2 1 (O) May be inoperative provided :
a) One cabin handset operates normally, b) Operative handset is located at an operative
flight attendant seat, and
c) Alternate communication procedures between the affected flight attendant station(s) are established and used.
NOTE:
Any station that operates normally may be used.
−50−7 Observer’s Audio Control
Panel B 1 0 May be inoperative except when required by a personin an official capacity. D 1 0 May be inoperative provided the seat is not required to
be available in an official capacity for extended periods of time.
−60−1 Static Dischargers D 25 19 May be missing provided no more than one is missing from each control surface cluster.
−70−1 Cockpit Voice Recorder A 1 0 May be inoperative provided:
a) The Flight Data Recorder is operative, and b) Repairs are made within three flight days. −80−1 ARCDU Radio Tuning
Function (Aircraft with at least one FMS installed)
C 2 1 (O) May be inoperative provided:
a) FMS Radio Tuning Function of the inoperative ARCDU in “FMS” mode is verified operative. b) The operative ARCDU Radio Tuning Function is
verified operative in “BOTH” or “FMS” mode.
23−6 Rev 7 Sep 09/2015
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
23 COMMUNICATION (CONT’D)
24 ELECTRICAL POWER
−20−1 AC GEN 1 and AC GEN 2
VOLT Indications (on ESID) C 6 0 May be inoperative provided:a) Associated electrical cautions are operative, b) Associated AC GEN LOAD Indication(s) are
operative, and
c) Both DC Generators are operative. −20−2 AC GEN 1 and AC GEN 2
LOAD Indications (on ESID) C 6 0 May be inoperative provided:a) Associated electrical cautions and/or warnings are operative,
b) Associated AC GEN VOLT Indications are operative, and
c) Both DC Generators are operative. −20−3 #1 AC GEN and #2 AC
GEN Caution Lights C 2 1 May be inoperative provided:a) Associated AC GEN VOLT and AC GEN LOAD Indications are operative and are periodically monitored during flight, and
b) Both AC Generators are verified operative prior to each flight.
−30−1 Transformer Rectifier Units
(TRUs) B 2 1 (M) May be inoperative provided:a) Both DC Starter/Generators are operative, and b) Associated TRU is deactivated.
−30−2 DC Generator Control Unit − Start / Termination Function
B 2 0 (O) May be inoperative provided the start is manually terminated at 50% NH.
−30−3 BATT °C Temperature
Indications C 3 0 (O) May be inoperative provided:a) The associated BAT HOT Warning Light(s) are verified operative, and
b) The associated DC BATT LOAD Indication(s) are verified operative.
−30−4
***
APU Generation System D 1 0 (M#) May be inoperative provided:a) The cause of the malfunction is determined, and b) Appropriate action is taken to ensure that nohazard exists.
D 1 0 May be inoperative provided the APU is considered inoperative and is not used.
Rev 6 Mar 26/2014 24−1
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
−30−5 DC GEN LOAD Indications C 2 1 (O) May be inoperative provided both DC Generators are operative.
C 2 1 (O) May be inoperative provided the inoperative Indication is associated with a failed DC Generator. −30−6 DC Starter/Generation
Systems B 2 1 (M#)(O) One GCU and/or Generator may beinoperative in the generation mode only (i.e. DC GEN caution light illuminated) provided:
a) The cause of the malfunctions is determined and appropriate action is taken to ensure that no hazard exists,
b) The failed DC Generator is switched OFF, and c) Both Transformer Rectifier Units (TRUs) are
verified operative, and
d) Operations are conducted in compliance with AFM Supplement 92, OPERATION WITH ONE DC GENERATOR INOPERATIVE.
−40−1 AC External Power System D 1 0 May be inoperative. −40−2 DC External Power System D 1 0 May be inoperative.
24−2 Rev 6 Mar 26/2014
Systems & Nos de Sequence système Numbers de série
1. Item− Article
2. Number installed− Nombre d’articles installés
3. Number required for dispatch− Nombre requis pour le départ
4. Remarks or Exceptions− Remarques ou exceptions
24 ELECTRICAL POWER (CONT’D)
25 EQUIPMENT AND FURNISHINGS
−10−1 Forward Observer Seat (including associated equipment)
B 1 0 (M) May be inoperative provided the seat is removed, stowed, or secured in the retracted position.
D 1 0 (M) May be inoperative provided:
a) The seat is not required to be occupied in an official capacity for extended periods of time, and b) The seat is removed, stowed, or secured in the
retracted position. −10−2 Pilot’s Seat Adjustments
1) Vertical Mode
Adjustment C 2 0 (M#) Vertical adjustment may be inoperative providedthe seat is secured in a position, which meets individual pilot requirements.
2) Fore/Aft Mode B 2 0 (M#) Fore/aft adjustment may be inoperative provided the seat is secured in a position, which meets
individual pilot requirements.
3) Crew Armrests C 4 0 (M#) May be inoperative provided the armrest(s) is (are) removed from the seat.
4) Lumber Support C 2 0 May be inoperative in the lowest position provided the